Energy index for aircraft maneuvers
a technology of energy index and aircraft, applied in the direction of aircraft traffic control, instruments, alarms, etc., can solve the problems of affecting the recovery of energy, and a second class of high energy arrivals in which recovery and subsequent stabilization are likely to be difficult or impossibl
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[0020]FIGS. 1A and 1B illustrate environments for an ascending aircraft (1A) and for a descending aircraft (1B) where the invention can be practiced. In FIG. 1A, an aircraft 11A is ascending, either after takeoff or in moving from a first flight altitude to a second flight altitude. The aircraft has an associated kinetic energy component KE(tn), measured or estimated or otherwise provided, at each of a first sequence {tn}n of two or more time values, and has an associated potential energy component PE(tn), measured or estimated or otherwise provided, at the first sequence {tn}n of time values. The aircraft kinetic energy and potential energy components are, respectively,
KE(t)=m(t)·v(t)2 / 2+ω·I·ω / 2, (1)
PE(t)=m(t)·g··h(t), (2)
where m(t) is the instantaneous mass (taking account of fuel consumption), I(t) is an instantaneous moment of inertia tensor for the aircraft, ω(t) is an aircraft rotation vector, computed with reference to a center of gravity or other selected location determin...
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